Life Prediction of Rocket Combustion-Chamber-Type Thermomechanical Fatigue Panels-Reference-Cited by-同舟云学术

Life Prediction of Rocket Combustion-Chamber-Type Thermomechanical Fatigue Panels

Published:2017-11 Issue:6 Volume:33 Page:1529-1542
ISSN:0748-4658
Container-title:Journal of Propulsion and Power
language:en
Short-container-title:Journal of Propulsion and Power

Author:

Thiede R. G.¹,Riccius J. R.¹,Reese S.²

Affiliation:

1. DLR, German Aerospace Center, D-74239 Hardthausen, Germany

2. RWTH Aachen University, D-52074 Aachen, Germany

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.B36361

Reference31 articles.

1. MillerR. W. “Cyclic Fatigue Analysis of Rocket Thrust Chambers: Volume 1—OFHC Copper Chamber Low Cycle Fatigue,” NASA CR-134641, June 1974.

2. QuentmeyerR. J. “Experimental Fatigue Life Investigations of Cylindrical Thrust Chambers,” NASA TM-X-73665, July 1977.

3. ArmstrongW. H. “Structural Analysis of Cylindrical Thrust Chambers—Volume 1,” NASA CR-159522, March 1979.

4. BadlaniM. L.PorowksiJ. S.O'DonnellW. J.PetersonD. B. “Development of a Simplified Procedure for Rocket Engine Thrust Chamber Life Prediction with Creep,” NASA CR-168261, March 1984.

5. Viscoplastic analysis of an experimental cylindrical thrust chamber liner

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